Contents and Arrangement

Automatic design of transonic airfoils to reduce the shock induced pressure drag, 1990 February

1 item

Collection Overview

Collection Description & Creator Information

Description:

Consists of technical reports from the Department of Mechanical and Aerospace Engineering.

Collection History

Access & Use

Access Restrictions:

Collection is open for research use.

Conditions for Reproduction and Use:

Single photocopies may be made for research purposes. For quotations that are fair use as defined under U. S. Copyright Law, no permission to cite or publish is required.

Credit this material:

Automatic design of transonic airfoils to reduce the shock induced pressure drag; Department of Mechanical and Aerospace Engineering Reports, ENG007, Technical and Scientific Reports, Engineering Library, Princeton University Library

Location:
Engineering Library
Engineering Library
Friend Center for Engineering Education
Princeton, NJ 08540, USA
(609) 258-3200
englib@princeton.edu

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